JPS59155530A - Combustion chamber structure of internal-combustion engine - Google Patents

Combustion chamber structure of internal-combustion engine

Info

Publication number
JPS59155530A
JPS59155530A JP58029165A JP2916583A JPS59155530A JP S59155530 A JPS59155530 A JP S59155530A JP 58029165 A JP58029165 A JP 58029165A JP 2916583 A JP2916583 A JP 2916583A JP S59155530 A JPS59155530 A JP S59155530A
Authority
JP
Japan
Prior art keywords
combustion chamber
spark plug
cylinder
exhaust port
port
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP58029165A
Other languages
Japanese (ja)
Other versions
JPS641648B2 (en
Inventor
Kenichi Sasaki
健一 佐々木
Mitsuru Takahashi
満 高橋
Yoshio Iwasa
岩佐 喜夫
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP58029165A priority Critical patent/JPS59155530A/en
Publication of JPS59155530A publication Critical patent/JPS59155530A/en
Publication of JPS641648B2 publication Critical patent/JPS641648B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/08Other engines characterised by special shape or construction of combustion chambers to improve operation with positive ignition
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2275/00Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/20SOHC [Single overhead camshaft]
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Abstract

PURPOSE:To prevent a spark plug from being fouled and misfiring from occurring due to the spark plug being directly hit by inflowing mixture by a structure wherein the spark plug is arranged at a position free from being directly hit by inflowing mixture and at the same time the velocity of mixture flow near the spark plug is fully raised by a guide wall formed along the peripheral edge of a combustion chamber. CONSTITUTION:A hemispherical combustion chamber 14 is concavedly arranged on a cylinder head 12. A suction passage 15 and an exhaust passage 16 are arranged in a crossflowing manner with respect to the combustion chamber 14 so as to connect to a suction port 17 and an exhaust port 18, both of which are respectively open to the combustion chamber 14. Further, the suction passage 15 points to a position deviated from the axis center of a cylinder. In this case, each spark plug 21 is positioned within a domain A, which is surrounded with a line l1 to connect the centers O1 of the respective suction ports 17 in the direction of line of cylinders, a line l2 to be normal to the line of cylinders and simultaneously tangent to an outer edge of the exhaust port 18, and the outer edges of the suction port 17 and of the exhaust port 18. Furthermore, a guide wall 22, which extends itself curvedly toward the inner peripheral side of a cylinder, is provided along the peripheral edge of the combustion chamber at a portion on the spark plug 21 side.

Description

【発明の詳細な説明】 この発明は、半球状の燃焼室に対し吸気通路および排気
通路がクロスフロー形に配置されてなる内燃機関の燃焼
室構造の改良に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an improvement in the structure of a combustion chamber of an internal combustion engine in which an intake passage and an exhaust passage are arranged in a cross-flow manner in a hemispherical combustion chamber.

比較的希薄な混合気による運転に適した燃焼室構造とし
て、半球状の燃焼室、に吸気通路および排気通路をクロ
ス70−形に配、置するとともに、上記吸気通路をシリ
ンダ軸心か゛ら一方に偏した位置に指向させて吸気スワ
ールを強化し、このスワールの利用により良好な燃焼を
図ったものがあるが、この場合一般に第1図(%公昭5
7−61884号公報)あるいは第2図(%公昭54−
10059号公報)に示すように、半球状燃焼室lにお
いて、吸気通路2の前方つまり吸気通路2が直接指向す
る位置に点火栓3を配置し、この点火栓3近傍の流速を
十分に確保するようにしている。
As a combustion chamber structure suitable for operation with a relatively lean air-fuel mixture, an intake passage and an exhaust passage are arranged in a cross 70-shape in a hemispherical combustion chamber, and the intake passage is placed on one side from the cylinder axis. There are some systems that strengthen the intake swirl by directing it to a biased position, and use this swirl to achieve good combustion.
7-61884) or Figure 2 (% Publication No. 1973-
As shown in Japanese Patent Publication No. 10059), in the hemispherical combustion chamber l, the ignition plug 3 is arranged in front of the intake passage 2, that is, at a position where the intake passage 2 is directly directed, and a sufficient flow velocity in the vicinity of the ignition plug 3 is ensured. That's what I do.

しかしながら、このように吸気通路2の前方に点火栓3
を配置すると、燃焼室1内に入いったばかシの混合気が
点火栓3を直撃することになり、該点火栓3が過冷とな
って燻ったり、あるいは液状燃料の付着によシ失火を生
じたシし易くなり、その結果運転性や燃料消費の悪化を
生じていた。
However, in this way, the ignition plug 3 is located in front of the intake passage 2.
If the fuel mixture enters the combustion chamber 1, it will directly hit the ignition plug 3, and the ignition plug 3 will become supercooled and smoke, or the liquid fuel may adhere to it, causing a misfire. This results in deterioration of drivability and fuel consumption.

特に吸気量の多い機関高速運転時において理論空燃比近
傍での運転が困難となるため、燃料消費が著しく悪化し
てしまう。
Particularly when the engine is operating at high speed with a large amount of intake air, it becomes difficult to operate near the stoichiometric air-fuel ratio, resulting in a significant increase in fuel consumption.

また、第2図の例では、吸気通路2の一部を案内壁4に
て覆うようにして、この案内壁4により混合気を点火栓
3側に向けているが、この場合上記案内壁4によって吸
′気流人時の抵抗が増大してしまい、機関の最高出力が
制約される欠点がある。
In the example shown in FIG. 2, a part of the intake passage 2 is covered with a guide wall 4, and the air-fuel mixture is directed toward the spark plug 3 by the guide wall 4. In this case, the guide wall 4 This has the disadvantage that the resistance during intake air flow increases, which limits the maximum output of the engine.

この発明は上記のような従来の問題に鑑みてなされたも
ので、点火栓を流入混合気の直撃を受けない位置に配置
せしめる一方、その近傍の流速を燃焼室周縁の案内壁に
より十分に高めるようにして、失火や燻りを確実に防止
し、燃料消費性能等の向上を図ることを目的とす−る。
This invention was made in view of the above-mentioned conventional problems, and while the ignition plug is placed in a position where it is not directly hit by the inflowing air-fuel mixture, the flow velocity in the vicinity is sufficiently increased by a guide wall around the periphery of the combustion chamber. In this way, the purpose is to reliably prevent misfires and smoldering, and improve fuel consumption performance, etc.

すなわち、この発明に係る2、丙燃機関の燃焼室構造は
、吸気口の中心をシ’) :’;’、ダ列方向に結ぶ線
と、排気口外縁、を通ってシリンダ列に直交する線と、
 ゛吸気口外縁および排気口外縁とで囲まれた領域に点
火栓が配設されるとともに、燃焼室周縁の点火栓側部分
にシリンダ内周側に張り出した案内壁が設けられたもの
である。
That is, the combustion chamber structure of the 2.C combustion engine according to the present invention has a line connecting the center of the intake port in the direction of the cylinder row and the outer edge of the exhaust port, and perpendicularly intersects the cylinder row. Lines and,
An ignition plug is disposed in an area surrounded by the outer edge of the intake port and the outer edge of the exhaust port, and a guide wall extending toward the inner circumferential side of the cylinder is provided on the ignition plug side portion of the periphery of the combustion chamber.

以下、この発明の一実施例を図面に基づいて詳細に説明
する。
Hereinafter, one embodiment of the present invention will be described in detail based on the drawings.

第3図および第4図において、11はシリンダブロック
、12idシリンダヘツド、13はロッカカバーであっ
て、′l:記シリンダヘッド■2には半球状の燃焼室1
4が凹設されているとともに、この燃焼室14に対し吸
気通路15および排気通路16がクロスフロー形に配置
されており、夫々燃焼室14に開口する吸気口17およ
び排気口18に連なっている。尚、19゜20は夫々上
記吸気口17 、排気口18を開閉する吸気弁および排
気弁である。ここで上記吸気通路15は、シリンダ軸心
から一方に偏した位i書を指向しており、具体的には第
3図に示すように、シリンダ列方向と略直交する方向で
かつ燃焼室14の接線方向に沿って形成されているとと
もに、吸気口17の直前部分が7リング軸心方向に向け
て僅かに湾曲された形状をなし、これにより燃焼室14
に矢印S方向の吸気スワールを生起せしめるようにしヤ
いる。
In FIGS. 3 and 4, 11 is a cylinder block, 12 is a cylinder head, 13 is a rocker cover, and 'l: cylinder head 2 has a hemispherical combustion chamber 1.
4 is recessed, and an intake passage 15 and an exhaust passage 16 are arranged in a cross-flow form with respect to the combustion chamber 14, and are connected to an intake port 17 and an exhaust port 18, respectively, which open into the combustion chamber 14. . Reference numerals 19 and 20 indicate an intake valve and an exhaust valve for opening and closing the intake port 17 and the exhaust port 18, respectively. Here, the intake passage 15 is oriented in a direction that is biased to one side from the cylinder axis, and specifically, as shown in FIG. The combustion chamber 14
This is done so as to cause an intake swirl in the direction of arrow S.

一方、各気筒に一つ備えられる点火栓21は、第3図に
示すように、吸気口17の中心OIをシリンダ列方向に
結ぶ線1.と、排気口18の外縁を通ってシリンダ列方
向に直交する線t2と、吸気・口17の外縁および排気
口18の外縁とで囲まれた領域A(第3図に斜線を施し
て示す部−分7)に配、置されているト尚、この点火栓
21はシリンダブロック12に対し、第4図に示すよう
に吸気側から脱着し得るもので、1熱性を保守の点で有
利になっている。
On the other hand, one ignition plug 21 is provided in each cylinder, as shown in FIG. 3, as shown in FIG. , a line t2 passing through the outer edge of the exhaust port 18 and perpendicular to the cylinder row direction, and the outer edge of the intake/port 17 and the outer edge of the exhaust port 18 (area A (the area shown with diagonal lines in FIG. 3). Furthermore, this spark plug 21 can be attached to and detached from the cylinder block 12 from the intake side as shown in FIG. It has become.

また、燃焼室14周縁の点火栓21側部分においては、
シリンダ内周側に弓状に張り出した案内壁22が設けら
れている。この案内壁22ば、吸気口17の中心01と
排気口18の中心02を結んだ線t3が燃焼室14周縁
と交わる2点の間にほぼ亘って形成されておシ、その幅
つまシ第4図の上下方向に沿った幅は、両端部から中央
部に向かって徐々に幅広となっている。これにより燃焼
室14は比較的コンパクトな形状となシ、とりわけ点火
栓21近傍の燃焼室深さを大きく確保しているCまた上
記案内壁22を形成することによって、実質的にスキッ
シュエリアBが形成されており、燃焼速度の向上に有効
なスキッシュの生成ヲ図っているc尚、このスキッシュ
エリアBの面積としては、シリンダボア断面積の0.1
5〜0.25程度が適尚である。
In addition, in the ignition plug 21 side portion of the periphery of the combustion chamber 14,
A guide wall 22 extending in an arcuate manner is provided on the inner peripheral side of the cylinder. This guide wall 22 is formed almost between two points where a line t3 connecting the center 01 of the intake port 17 and the center 02 of the exhaust port 18 intersects with the periphery of the combustion chamber 14, and its width is The width along the vertical direction in FIG. 4 gradually becomes wider from both ends toward the center. As a result, the combustion chamber 14 has a relatively compact shape, and in particular, the depth of the combustion chamber near the spark plug 21 is ensured to be large.Furthermore, by forming the guide wall 22, the squish area B is substantially reduced. The area of this squish area B is 0.1 of the cross-sectional area of the cylinder bore.
Approximately 5 to 0.25 is appropriate.

また、第5図には上記吸気通路】5から混合気を供給す
る燃料供給機構の一例として燃料噴射装置の概略を示し
てあシ、これは、吸気マニホルド3】に燃料噴射弁32
ヲ設けるとともに、エアフローメータ331機関回転数
センサ34,02センサ35.冷却水温センサ36.ス
ロットルスイッチ37等の各種信号に基づいて制御回路
38がその噴射量をフィードバック制御する構成であっ
て、略理論空燃比に近い比較的希薄々混合気を上記吸気
通路15に供給している。
FIG. 5 schematically shows a fuel injection device as an example of a fuel supply mechanism that supplies air-fuel mixture from the intake manifold 3.
In addition, an air flow meter 331, engine speed sensor 34, 02 sensor 35. Cooling water temperature sensor 36. The control circuit 38 feedback-controls the injection amount based on various signals from the throttle switch 37 and the like, and supplies a relatively lean air-fuel mixture close to the stoichiometric air-fuel ratio to the intake passage 15.

さて上記のように構成された燃焼室構造において、吸入
混合気は吸気道−路15に案、内されて燃焼室14の略
接線方向に流入し、燃焼室14内に矢印S方向のスワー
ルを生起せしめる。このとき、上記吸気通路15が吸気
口17の直前部分で若干湾曲しているため、混合気流は
シリンダボア壁を直撃することがなく、該ボア壁に沿っ
て清らかに流れ、従って流入抵抗は小さい。また吸気口
17と点火栓21との位蓋関係から明らかなように、流
入混合気が点火栓21を直撃することはなく、シかも混
合気中の液状燃料は吸気通路15の湾曲によって吸気口
17のシリンダ外周側に多く偏在するため、その反対側
に位I度する点火栓21には当ることがない。
Now, in the combustion chamber structure configured as described above, the intake air-fuel mixture is guided into the intake path 15 and flows into the combustion chamber 14 in a substantially tangential direction, creating a swirl in the combustion chamber 14 in the direction of arrow S. cause it to occur. At this time, since the intake passage 15 is slightly curved in front of the intake port 17, the mixed air flow does not directly hit the cylinder bore wall and flows cleanly along the bore wall, so that the inflow resistance is small. Furthermore, as is clear from the positional relationship between the intake port 17 and the spark plug 21, the incoming air-fuel mixture does not directly hit the spark plug 21, and the liquid fuel in the air-fuel mixture may be absorbed into the intake port by the curvature of the intake passage 15. Since most of the spark plugs are unevenly distributed on the outer peripheral side of the cylinder 17, they do not hit the spark plug 21 located on the opposite side.

一方、燃焼室14内に生じた♂ワールSは、排気口18
近傍から案内壁22に沿って流れる結果、その流速が高
められる。すなわち点火栓21近傍での流動を活発化し
て比較的希薄fX混合気に対する確実な着火゛を可能と
し、かつ火炎伝播を速めて燃焼を安定化し得る。また前
述したように燃焼室14が案内壁22の形成によってコ
ンパクトな形状上なるために、スワールの強化と相俟っ
てノッキングが発生しにくくなり、高圧縮比化(例えば
91〜94程度)や点火時期の進角が可能となる。
On the other hand, the male whirl S generated in the combustion chamber 14 is removed from the exhaust port 18.
As a result of flowing along the guide wall 22 from the vicinity, the flow velocity is increased. That is, by activating the flow near the spark plug 21, it is possible to reliably ignite a relatively lean fX mixture, and it is also possible to speed up flame propagation and stabilize combustion. In addition, as mentioned above, since the combustion chamber 14 has a compact shape due to the formation of the guide wall 22, knocking is less likely to occur due to the strengthened swirl, and a high compression ratio (for example, about 91 to 94) can be achieved. It is possible to advance the ignition timing.

従って、これらの相乗によって機関の失火限界空燃比は
20以上に高められ、例えば高速時において理論空燃比
近傍で運転することが十分に可能となり、上記の高圧縮
比化や点火時期進角とともに、燃料消費の大幅な改善が
図れる。
Therefore, the misfire limit air-fuel ratio of the engine is increased to 20 or more due to the synergistic effect of these factors, making it possible to operate near the stoichiometric air-fuel ratio at high speeds. Significant improvement in fuel consumption can be achieved.

以上の説明で明らか々ように、この発明に係る内燃機関
の燃焼室構造によれば、流入徂合気の直撃による点火栓
の燻シや失火を防止でき、比較的希Rな混合気を用いて
良、好な燃焼、を行ゎせることが可能となり、燃料消費
性能ならびに排気特性等の一層の改善を図ることができ
る。
As is clear from the above explanation, according to the combustion chamber structure of the internal combustion engine according to the present invention, it is possible to prevent the ignition plug from smoldering or misfire due to direct impact of the inflowing ai, and to use a relatively rare mixture of R. This makes it possible to achieve better fuel efficiency and better combustion, making it possible to further improve fuel consumption performance and exhaust characteristics.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図および第2図は夫々従来の燃焼室構造の一例を示
す平面図、第3図はこの発明に係る燃焼室構造を示す平
面図、第4図は同断面図、第5図はその燃料供給機構の
一例を示す構成説明図である。 l2・・・シリンダヘッド、14・■燃焼室、150・
吸気通路、16・・・排気通路、17・・・吸気口、1
8−・・・排気口、21−骨や点火栓、22・・・案内
壁。 第1図 第2図 第4図 第5図
1 and 2 are plan views showing an example of a conventional combustion chamber structure, FIG. 3 is a plan view showing a combustion chamber structure according to the present invention, FIG. 4 is a sectional view thereof, and FIG. 5 is a plan view thereof. FIG. 2 is a configuration explanatory diagram showing an example of a fuel supply mechanism. l2...Cylinder head, 14・■Combustion chamber, 150・
Intake passage, 16...Exhaust passage, 17...Intake port, 1
8-... Exhaust port, 21- Bones and spark plugs, 22... Guide wall. Figure 1 Figure 2 Figure 4 Figure 5

Claims (1)

【特許請求の範囲】[Claims] (1)吸気口および排気口を備えた半球状の燃焼室に対
し吸気通路および排気通路がクロスフロー形に配置され
、かつ上記吸気通路がシリンダ軸心から一方に偏した位
置を指向してなる内燃機関の燃焼室構造において、吸気
口の中心をシリンダ列方向に結ぶ線と、排気口外縁を通
ってシリンダ列に直交する線と、吸気口外縁および排気
口外縁とで囲まれた領域に点火栓が配設されるとともに
、燃焼室周縁の点火栓側部分に、シリンダ内周側に張り
出した案内壁が設けられてなることを特徴とする内燃機
関の燃焼室構造。
(1) An intake passage and an exhaust passage are arranged in a cross-flow shape in a hemispherical combustion chamber equipped with an intake port and an exhaust port, and the intake passage is oriented toward a position offset to one side from the cylinder axis. In the combustion chamber structure of an internal combustion engine, ignition occurs in an area surrounded by a line connecting the center of the intake port in the direction of the cylinder row, a line passing through the outer edge of the exhaust port and perpendicular to the cylinder row, and the outer edge of the intake port and the outer edge of the exhaust port. A combustion chamber structure for an internal combustion engine, characterized in that a plug is provided, and a guide wall extending toward the inner circumferential side of the cylinder is provided on the ignition plug side portion of the periphery of the combustion chamber.
JP58029165A 1983-02-23 1983-02-23 Combustion chamber structure of internal-combustion engine Granted JPS59155530A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP58029165A JPS59155530A (en) 1983-02-23 1983-02-23 Combustion chamber structure of internal-combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58029165A JPS59155530A (en) 1983-02-23 1983-02-23 Combustion chamber structure of internal-combustion engine

Publications (2)

Publication Number Publication Date
JPS59155530A true JPS59155530A (en) 1984-09-04
JPS641648B2 JPS641648B2 (en) 1989-01-12

Family

ID=12268631

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58029165A Granted JPS59155530A (en) 1983-02-23 1983-02-23 Combustion chamber structure of internal-combustion engine

Country Status (1)

Country Link
JP (1) JPS59155530A (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS56115817A (en) * 1980-02-14 1981-09-11 Nissan Motor Co Ltd Combustion chamber for spark igniting engine
JPS57203818A (en) * 1981-06-09 1982-12-14 Nissan Motor Co Ltd Spark-ignition type internal-combustion engine

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS56115817A (en) * 1980-02-14 1981-09-11 Nissan Motor Co Ltd Combustion chamber for spark igniting engine
JPS57203818A (en) * 1981-06-09 1982-12-14 Nissan Motor Co Ltd Spark-ignition type internal-combustion engine

Also Published As

Publication number Publication date
JPS641648B2 (en) 1989-01-12

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